Mach Number in Rocket Propulsion Formulas

Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound. And is denoted by M.

Rocket Propulsion formulas that make use of Mach Number

fxExit Velocity given Mach Number and Exit TemperatureGo

fxRocket Exit TemperatureGo

fxRocket Exit PressureGo

fxCompressible Area RatioGo

fxMass Flow Rate through EngineGo

What is the Mach Number?

Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.

Can the Mach Number be negative?

{YesorNo}, the Mach Number, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

Let Others Know

✖

Copied!